THOR AGENA D R/B
NORAD 2825
Rocket Body
LEO
1967-053B
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
898 km
Apogee
905 km
Inclination
70.0°
Period
103.0 min
Mean Motion
13.97742564 rev/day
TLE Epoch
2026-09-15 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude902 km
Orbital Velocity26,652 km/h
Velocity7.40 km/s
Orbital Period103 minutes
Orbits / Day13.98
Eccentricity0.0005
Semi-Major Axis7,273 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1967-05-31
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1967-053B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
THOR AGENA D R/B is a spent rocket body associated with United States, launched on 1967-05-31 from Vandenberg Space Force Base, United States on the NRL PL160 launch. After more than 59 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 898 km and 905 km with an inclination of 70.0°. It travels at approximately 26,652 km/h (7.40 km/s), completing one full orbit every 103 minutes — that’s roughly 13.98 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Spent rocket bodies like THOR AGENA D R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
THOR AGENA D R/B orbits at an average altitude of 902 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of THOR AGENA D R/B’s average altitude, there are currently 264 active payloads and 1,584 tracked debris or rocket body fragments. With an inclination of 70.0°, THOR AGENA D R/B passes over latitudes between 70.0°N and 70.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 13,206 active satellites in total, of which 112 share a similar altitude band with THOR AGENA D R/B.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
THOR AGENA D R/B orbits in Low Earth Orbit (LEO) at altitudes between 898 km (perigee) and 905 km (apogee), with an average altitude of approximately 902 km. It completes one orbit every 103 minutes, travelling at approximately 26,652 km/h (16,561 mph).
THOR AGENA D R/B (NORAD ID 2825) is a spent rocket body — the upper stage of a launch vehicle attributed to United States. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
THOR AGENA D R/B was launched on 1967-05-31 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks THOR AGENA D R/B (NORAD ID 2825) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
THOR AGENA D R/B travels at approximately 26,652 km/h (16,561 mph) — roughly 7.40 km/s. It completes 13.98 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.